AbstractIntegratedPropagator

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total28 of 92696%4 of 5492%5666200139
integrateDynamics(AbsoluteDate)1416992%11191%1724001
propagate(AbsoluteDate)51979%1375%131501
secondary(SpacecraftState)35094%1375%1311001
secondaryDerivative(SpacecraftState)35094%1375%1311001
isMeanOrbit()30%n/a111111
propagate(AbsoluteDate, AbsoluteDate)91100%8100%0501801
convert(ODEStateAndDerivative)74100%4100%0301501
createInitialState(SpacecraftState)57100%4100%0301001
getManagedAdditionalStates()41100%2100%020601
convert(SpacecraftState)35100%n/a010601
AbstractIntegratedPropagator(ODEIntegrator, PropagationType)32100%n/a010901
isAdditionalStateManaged(String)27100%6100%040701
addAdditionalDerivativesProvider(AdditionalDerivativesProvider)26100%2100%020601
setAttitudeProvider(AttitudeProvider)24100%n/a010501
createODE(ODEIntegrator, ODEState)24100%2100%020501
setOrbitType(OrbitType)21100%n/a010401
setPositionAngleType(PositionAngle)21100%n/a010401
setMu(double)21100%n/a010401
setUpUserEventDetectors()18100%2100%020401
setUpEventDetector(ODEIntegrator, EventDetector)14100%n/a010501
getEphemerisGenerator()13100%n/a010301
initMapper()11100%n/a010201
addAdditionalEquations(AdditionalEquations)9100%n/a010201
addEventDetector(EventDetector)6100%n/a010201
setResetAtEnd(boolean)4100%n/a010201
getOrbitType()4100%n/a010101
getPositionAngleType()4100%n/a010101
getMu()4100%n/a010101
getAdditionalDerivativesProviders()4100%n/a010101
getEventsDetectors()4100%n/a010101
clearEventsDetectors()4100%n/a010201
getPropagationType()3100%n/a010101
getCalls()3100%n/a010101
getInitialIntegrationState()3100%n/a010101
getIntegrator()3100%n/a010101
getBasicDimension()2100%n/a010101
setUpStmAndJacobianGenerators()100%n/a010101
beforeIntegration(SpacecraftState, AbsoluteDate)100%n/a010101
afterIntegration()100%n/a010101